A fuel tank with a suction system, comprising a flexible hose comprising first and second extremities, the second extremity comprising an orifice configured to be connected to a first orifice of a first pipeline via a connection point. The first extremity of the flexible hose is fastened to a floating system and comprises at least one orifice, such that the orifice is a suction point always able to supply the engine from an upper layer of fuel available inside the tank, to avoid water and dirt from the lower layer.
FUEL TANK WITH SUCTION SYSTEM
2019-06-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |